• DocumentCode
    3112367
  • Title

    Robust Stability in a Classical and Modern Context

  • Author

    Halsey, Kelvin M.

  • Author_Institution
    Department of Electrical and Electronic Engineering, University of Melbourne, Melbourne, VIC 3010, Australia (e-mail: kmhalsey@ieee.org).
  • fYear
    2005
  • fDate
    12-15 Dec. 2005
  • Firstpage
    2308
  • Lastpage
    2313
  • Abstract
    Excluding the open loop gain of a feedback system from a region about the origin of the Nichols chart yields a natural guarantee of robust stability which is commonly used in the analysis of flight control systems. This paper shows that a generalised form of M-circle, based upon a contour of constant |S| + |T|, is symmetrical on the Nichols chart and yields a stability margin consistent with the gain and phase margin requirements of the USAF. This new margin, motivated on purely classical grounds, is shown to be equal to the robust stability margin associated with the loopshaping design procedure of McFarlane and Glover. A corresponding interpretation is obtained for the multivariable case.
  • Keywords
    Aerospace control; Australia; Control system analysis; Feedback loop; Frequency; Kelvin; Low-frequency noise; Robust stability; Stability criteria; Transfer functions;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2005 and 2005 European Control Conference. CDC-ECC '05. 44th IEEE Conference on
  • Print_ISBN
    0-7803-9567-0
  • Type

    conf

  • DOI
    10.1109/CDC.2005.1582506
  • Filename
    1582506